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FR2615616B1 - METHOD AND DEVICE FOR DETERMINING THE PASSAGE - Google Patents

METHOD AND DEVICE FOR DETERMINING THE PASSAGE

Info

Publication number
FR2615616B1
FR2615616B1 FR888806646A FR8806646A FR2615616B1 FR 2615616 B1 FR2615616 B1 FR 2615616B1 FR 888806646 A FR888806646 A FR 888806646A FR 8806646 A FR8806646 A FR 8806646A FR 2615616 B1 FR2615616 B1 FR 2615616B1
Authority
FR
France
Prior art keywords
passage
determining
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Fee Related
Application number
FR888806646A
Other languages
French (fr)
Other versions
FR2615616A1 (en
Inventor
Karl-Heinz Lachmann
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Diehl Verwaltungs Stiftung
Original Assignee
Diehl GmbH and Co
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Diehl GmbH and Co filed Critical Diehl GmbH and Co
Publication of FR2615616A1 publication Critical patent/FR2615616A1/en
Application granted granted Critical
Publication of FR2615616B1 publication Critical patent/FR2615616B1/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41—WEAPONS
    • F41G—WEAPON SIGHTS; AIMING
    • F41G7/00—Direction control systems for self-propelled missiles
    • F41G7/34—Direction control systems for self-propelled missiles based on predetermined target position data
    • F41G7/343—Direction control systems for self-propelled missiles based on predetermined target position data comparing observed and stored data of target position or of distinctive marks along the path towards the target
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41—WEAPONS
    • F41G—WEAPON SIGHTS; AIMING
    • F41G7/00—Direction control systems for self-propelled missiles
    • F41G7/008—Combinations of different guidance systems

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • General Engineering & Computer Science (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
FR888806646A 1987-05-18 1988-05-18 METHOD AND DEVICE FOR DETERMINING THE PASSAGE Expired - Fee Related FR2615616B1 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE19873716606 DE3716606A1 (en) 1987-05-18 1987-05-18 METHOD AND DEVICE FOR DETERMINING THE APOGAE PASSAGE

Publications (2)

Publication Number Publication Date
FR2615616A1 FR2615616A1 (en) 1988-11-25
FR2615616B1 true FR2615616B1 (en) 1992-12-11

Family

ID=6327793

Family Applications (1)

Application Number Title Priority Date Filing Date
FR888806646A Expired - Fee Related FR2615616B1 (en) 1987-05-18 1988-05-18 METHOD AND DEVICE FOR DETERMINING THE PASSAGE

Country Status (3)

Country Link
US (1) US4856733A (en)
DE (1) DE3716606A1 (en)
FR (1) FR2615616B1 (en)

Families Citing this family (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE4325218C2 (en) * 1993-07-28 1998-10-22 Diehl Stiftung & Co Artillery missile and method for increasing the performance of an artillery missile
IL117589A (en) * 1996-03-21 2001-10-31 Israel Aircraft Ind Ltd Guidance system for air-to-air missiles
WO2000049361A1 (en) * 1999-02-16 2000-08-24 Mashinostroitelnoe Konstruktorskoebjuro 'fakel' Method for the aeroballistic control of an aerodynamic aircraft
WO2007089243A2 (en) * 2005-02-07 2007-08-09 Bae Systems Information And Electronic Systems Integration Inc. Optically guided munition control system and method
US7503521B2 (en) * 2005-02-07 2009-03-17 Bae Systems Information And Electronic Systems Integration Inc. Radiation homing tag
US20080029641A1 (en) * 2005-02-07 2008-02-07 Bae Systems Information And Electronic Systems Three Axis Aerodynamic Control of Guided Munitions
WO2006086528A2 (en) * 2005-02-07 2006-08-17 Bae Systems Information And Electronic Systems Integration Inc. Ballistic guidance control for munitions
WO2006088687A1 (en) * 2005-02-07 2006-08-24 Bae Systems Information And Electronic Systems Integration Inc. Optically guided munition
US8130137B1 (en) 2005-07-26 2012-03-06 Lockheed Martin Corporation Template updated boost algorithm
US20070157226A1 (en) * 2005-12-21 2007-07-05 Raghavendra Misra Segmentation and communication of live-action sporting event data apparatus and method
US8134103B2 (en) * 2006-12-27 2012-03-13 Lockheed Martin Corporation Burnout time estimation and early thrust termination determination for a boosting target
DE102007060567B4 (en) 2007-12-15 2009-08-27 Junghans Microtec Gmbh Safety device for an igniter of a projectile
US9677864B1 (en) 2014-11-19 2017-06-13 Orbital Research Inc. Closed, self-contained ballistic apogee detection module and method
US11629518B2 (en) 2017-02-28 2023-04-18 Hummingbird Kinetics LLC Tuned liquid damper with a membrane liquid-gas interface
DE102019007315B3 (en) * 2019-10-21 2020-11-05 Stefan Barth Combination rotation lever with screw conveyor for small hydropower plants

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3332642A (en) * 1965-07-28 1967-07-25 Michael A Halling Summit sensing guidance initiation device
US4589610A (en) * 1983-11-08 1986-05-20 Westinghouse Electric Corp. Guided missile subsystem
US4606514A (en) * 1984-08-10 1986-08-19 Martin-Marietta Corporation Method for homing a projectile onto a target and for determining the ballistic trajectory thereof as well as arrangements for implementing the method

Also Published As

Publication number Publication date
DE3716606C2 (en) 1989-03-02
DE3716606A1 (en) 1988-12-08
FR2615616A1 (en) 1988-11-25
US4856733A (en) 1989-08-15

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Legal Events

Date Code Title Description
ST Notification of lapse